What was found
INSPECTION FOUND A .5 INCH CRACK IN C-2 DOOR OUTER SKIN. THE CRACK WAS LOCATED AT THE AFT UPPER CORNER OF C-2 DOOR HANDLE CUTOUT. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-30-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .5 INCH CRACK IN C-2 DOOR OUTER SKIN. THE CRACK WAS LOCATED AT THE AFT UPPER CORNER OF C-2 DOOR HANDLE CUTOUT. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-30-01.